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US9051633B2 - Aluminum alloy welded member - Google Patents

Aluminum alloy welded member Download PDF

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US9051633B2
US9051633B2 US13/640,120 US201013640120A US9051633B2 US 9051633 B2 US9051633 B2 US 9051633B2 US 201013640120 A US201013640120 A US 201013640120A US 9051633 B2 US9051633 B2 US 9051633B2
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aluminum alloy
mass
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welded
welded component
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US20130029114A1 (en
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Yoshikazu Ozeki
Toshihiko Fukuda
Kenji Katou
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Sumitomo Light Metal Industries Ltd
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Sumitomo Light Metal Industries Ltd
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium as the next major constituent
    • C22C21/08Alloys based on aluminium with magnesium as the next major constituent with silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium as the next major constituent
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/12Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/12Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding
    • B23K20/122Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding using a non-consumable tool, e.g. friction stir welding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/22Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded
    • B23K20/233Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded without ferrous layer
    • B23K20/2336Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded without ferrous layer both layers being aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00Materials to be soldered, welded or cut
    • B23K2103/08Non-ferrous metals or alloys
    • B23K2103/10Aluminium or alloys thereof
    • B23K2203/10
    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D11/00Electrolytic coating by surface reaction, i.e. forming conversion layers
    • C25D11/02Anodisation
    • C25D11/04Anodisation of aluminium or alloys based thereon
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24802Discontinuous or differential coating, impregnation or bond [e.g., artwork, printing, retouched photograph, etc.]

Definitions

  • the present invention relates to an aluminum alloy welded component which may be used, e.g., in the manufacture of vehicular wheels and housings, and which has an anodized coating formed after end portions of one or more aluminum alloy members have been integrally welded by friction stir welding.
  • a plate-shaped aluminum alloy member 11 is bent into a cylindrical shape, and then end portions 12 thereof are butted against each other and integrally welded by friction stir welding 13 therebetween, to make a cylindrical component 14 .
  • both ends are flared to make the wheel.
  • a coating is formed by anodizing the design surface, which is the surface on the opposite side of the welded section.
  • a side member 3 and a cover member 2 which are both made from an aluminum alloy material, are integrally welded by friction stir welding to form a joint 5 .
  • the integrally-welded side member 3 and the cover member 2 are face milled to smoothen the outer surface of the welded side, including the welded section 4 , and then a coating 6 is formed on the design surface by anodizing to improve corrosion and wear resistance properties.
  • color tone variations may occur in the coating 6 formed on the design surface due to differences of the crystal grain sizes between the portions corresponding to the welded section 4 and other non-welded portions.
  • the crystal grain sizes are equalized by performing a heat treatment prior to anodizing, the color tone variations, which exist between the portion corresponding to the welded section in the coating of the aluminum alloy welded component and the other portions, may not be sufficiently reduced.
  • Patent Reference 1 Japanese Patent Application Publication No. 2003-225780
  • Patent Reference 2 Japanese Patent Application Publication No. 2003-230970
  • the cross-sectional microstructures of the welded section obtained by friction stir welding and the other non-welded portions of the aluminum alloy welded component were first compared in detail using an optical microscope. As a result, it was found that second phase particles of 2 ⁇ m or larger in the welded section were decreased because the second phase particles made of coarse Al—Fe—Si particles were finely pulverized by the stirring; second phase particles of 5 ⁇ m or larger were scarcely found. Then, a comparison investigation was performed on the portion in the design surface that forms the coating, which is equivalent to the welded section (hereinafter, called “welded section equivalent portion”), and the other non-welded portions.
  • welded section equivalent portion the portion in the design surface that forms the coating
  • the second phase particles including the coarse second phase particles, were inhomogeneously dispersed in the welded section equivalent portion.
  • color tone variations could be recognized in the coating, because variations in pit formation caused by etching during the anodizing treatment become larger.
  • color tone variations in the anodized coating of the aluminum alloy welded component attributable to the inhomogeneous dispersion of second phase particles at the welded section equivalent portion are preferably eliminated in the manner that will be further described below.
  • an aluminum alloy welded component is formed from one or more aluminum alloy members comprised of Mg: 0.3% to 6.0% (mass %, hereinafter the same), Cu: 0.2% or less, Si: 0.1% or less, Fe: 0.1% or less, the balance being Al and inevitable impurities.
  • the grain size of second phase particles dispersed within the aluminum alloy member(s) is 5 ⁇ m or less when observed with an optical microscope.
  • mutually-facing end surfaces of the aluminum alloy member(s) are integrally welded by friction stir welding so as to form a welded section, and a coating is formed by anodizing a surface of the welded section, or an opposite surface thereof.
  • the inhomogeneous dispersion of the second phase particles is suppressed, even if the aluminum alloy member(s) is (are) welded in the welded section equivalent portion by friction stir welding and even as compared to the other portions.
  • variations in pit formation caused by etching during anodizing between the welded section equivalent portion and the other portions decrease, it is possible to prevent color tone variations in the coating of the aluminum alloy welded component.
  • Mg contained in the aluminum alloy welded component contributes to adjusting the strength of vehicular wheels and housings, which are shown in FIGS. 1-3 . Therefore, because the strength is insufficient with less than 0.3% Mg and shaping becomes difficult with more than 6.0% Mg, while Mg should preferably be 0.3% to 6.0%, for a good balance of ensuring strength and ease of shaping, it is more preferably 1.0% to 6.0%, and even more preferably 2.0% to 6.0%.
  • Cu contributes to homogenizing the color tone of the entire coating after anodizing. Therefore, because the coating after anodizing will be turbid with more than 0.2% Cu due to the effect of fine precipitates of Al—Cu particles, 0.2% or less Cu is included according to the present invention.
  • Si and Fe form second phase particles made of Al—Fe—Si. If the amounts of Si and Fe are each more than 0.1%, coarse second phase particles of Al—Fe—Si that exceed a grain size of 5 ⁇ m can easily form. Therefore, although the coarse second phase particles are preferably pulverized in the welded section during friction stir welding, the second phase particles, including the coarse particles, are inhomogeneously dispersed in the welded section equivalent portion by the agitation of the friction stir welding. As a result, variations in pit formation caused by the etching during anodizing increase due to the second phase particles being inhomogeneously dispersed in the welded section equivalent portion as compared to other portions, and color tone variations in the coating are caused. Therefore, according to the present teachings, the amounts of Si and Fe are each preferably 0.1% or less and more preferably 0.07% or less.
  • the second phase particles within the aluminum alloy member(s) are dispersed in the aluminum alloy welded component in an amount of 10000 particles/mm 2 or less when observed using an optical microscopic. If the second phase particles dispersed within the aluminum alloy members are thus reduced, the dispersion of the second phase particles in the welded section equivalent portion caused by the agitation during the friction stir welding can be minimized as compared to the other portions. As a result, variations in pit formation caused by the etching during anodizing become less, and the color tone variation in the coating can be eliminated more reliably.
  • the inhomogeneous dispersion of the second phase particles is a cause of the color tone variation in the coating formed by anodizing the above-described aluminum alloy welded component. Therefore, if the distribution density of the second phase particles when observed using an optical microscope is greater than 10000 particles/mm 2 , the dispersion of the second phase particles in the welded section equivalent portion during friction stir welding becomes more inhomogeneous as compared to the other portions. Therefore, variations in pit formation caused by the etching during anodizing increasingly cause color tone variations in the coating.
  • the quantity of second phase particles is reduced to prevent their inhomogeneous dispersion in the welded section equivalent portion, and the distribution density of the second phase particles when observed using an optical microscope is set to 10000 particles/mm 2 or less.
  • anodized coating is formed on the side of the welded section surface or the surface opposite thereof, a higher quality anodized product can be achieved by limiting the amounts of metal(s) that may form second phase particles and by limiting the grain size of the second phase particles in both the welded section equivalent portion and the other portions.
  • a uniform coating is thus formed that reliably eliminates color tone variations caused by the inhomogeneous dispersion of the second phase particles. Further, by appropriately setting the distribution density of the second phase particles, the elimination of color tone variations preferably can be achieved more reliably.
  • FIGS. 1 and 2 show a process for making a vehicle wheel.
  • FIG. 3 shows a housing having an anodized coating.
  • the objective i.e. to eliminate color tone variations existing between the welded section equivalent portion and the other portions in the coating of the aluminum alloy welded component welded by friction stir welding, is realized by limiting the amounts of Si and Fe that form second phase particles, and by limiting the grain sizes of the second phase particles. Further, by preferably also limiting the distribution density of the second phase particles, the objective can be realized in a more reliable manner.
  • inventive examples and the comparative examples were obtained by producing an ingot according to a semi-continuous casting process, homogenizing, forming plates having a thickness of 2.5 mm by hot rolling and cold rolling and then annealing to the O-temper (full-softening material).
  • Two plates each having a size of 100 mm in width ⁇ 200 mm in length were prepared. Longitudinal end surfaces thereof were butted with each other and friction stir welded.
  • the tool revolutions per minute were 500 rpm, the welding speed was 800 mm/min., the tool shoulder diameter was 7 mm, and the probe diameter was 3 mm.
  • the longitudinal end surfaces of the aluminum alloy members of the inventive materials 1 , 2 , and 3 serving as examples of the present invention, as well as the 5052 Materials 1 and 2 serving as the comparative examples, were integrally welded by friction stir welding along abutted portions to form a welded section; after welding, 0.5 mm of the surface layer of the welded surface, including the welded section, was removed using a milling machine, then a rough surface finish was prepared by shot blasting and an anodized coating having a thickness of 10 ⁇ m was formed by anodizing with sulfuric acid.
  • microstructures were observed after removal of 0.5 mm by face milling in the welded section equivalent portion and the other portions of the inventive materials 1 , 2 , and 3 according to the examples of the invention and the 5052 Materials 1 and 2 of the comparative examples. After buffing and then etching with 5% hydrogen fluoride, the microstructures were magnified 400 times using an optical microscope, and the number of particles per 1 mm 2 was obtained by measuring using an image analysis at 1 ⁇ m dot pitch grain size.
  • the second phase particles were homogeneously dispersed in the welded section equivalent portion on the opposite surface as compared to the other portions.
  • inventive material 1 the largest particle diameter was 5 ⁇ m, and the distribution density of the second phase particles equal to 5 ⁇ m or smaller was 7350 particles/mm 2 ; in inventive material 2 , the largest particle diameter was 4 ⁇ m, and the distribution density of the second phase particles equal to 4 ⁇ m or smaller was 2310 particles/mm 2 ; in inventive material 3 , the largest particle diameter was 5 ⁇ m, and the distribution density of the second phase particles equal to 5 ⁇ m or smaller was 4150 particles/mm 2 .
  • the second phase particles were inhomogeneously dispersed in the welded section equivalent portion as compared to the other portions.
  • the largest particle diameter was 6 ⁇ m, and the distribution density of the second phase particles equal to 6 ⁇ m or smaller was 6170 particles/mm 2 ; in 5052 Material 2 , the largest particle diameter was 7 ⁇ m, and the distribution density of the second phase particles equal to 7 ⁇ m or smaller was 8620 particles/mm 2 .
  • Inventive material 4 was used as the inventive material and 5052 Material 3 containing a greater amount of Fe was used as the 5052 Material (comparative example).
  • the chemical compositions are shown below in Table 2. The materials for testing were produced and evaluated by the same production and evaluation methods as mentioned above.
  • inventive material 4 exhibited neither color tone variations nor streak patterns in the welded section equivalent portion after the anodizing, the largest particle diameter was 4 ⁇ m, and the distribution density of the second phase particles equal to 4 ⁇ m or smaller was 2390 particles/mm 2 .
  • the 5052 Material 3 exhibited color tone variations in the welded section equivalent portion after anodizing, the second phase particles were inhomogeneously dispersed in the welded section equivalent portion thereof as compared to the other portions, the largest particle diameter was 8 ⁇ m, and the distribution density of the second phase particles equal to 8 ⁇ m or smaller was 11670 particles/mm 2 .

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Abstract

An aluminum alloy material is welded by performing friction stir welding to form a welded section in an aluminum alloy welded component. The aluminum alloy material contains Mg: 0.3-6.0% (mass %, hereinafter the same), Cu: 0.2% or less, Si: 0.1% or less, Fe: 0.1% or less, the balance being Al and inevitable impurities. Second phase particles dispersed in the aluminum alloy material have a grain size of 5 μm or less as observed with an optical microscopic. Because the second phase particles are homogeneously dispersed in a welded section equivalent portion of the aluminum alloy welded component as compared to other portions, variations in pit formation caused by etching during anodizing are reduced, thereby eliminating color tone variations in the anodized coating formed on the aluminum alloy welded component.

Description

CROSS-REFERENCE
This application is the US national stage of International Patent Application No. PCT/JP2010/068226 filed on Oct. 8, 2010.
TECHNICAL FIELD
The present invention relates to an aluminum alloy welded component which may be used, e.g., in the manufacture of vehicular wheels and housings, and which has an anodized coating formed after end portions of one or more aluminum alloy members have been integrally welded by friction stir welding.
BACKGROUND ART
In the past, aluminum alloy welded components have been used in the manufacture of vehicular wheels and housings due to their light weight properties. For example, in the manufacture of vehicular wheels as shown in FIGS. 1 and 2, a plate-shaped aluminum alloy member 11 is bent into a cylindrical shape, and then end portions 12 thereof are butted against each other and integrally welded by friction stir welding 13 therebetween, to make a cylindrical component 14. In addition, both ends are flared to make the wheel. Furthermore, to improve the corrosion resistance and the wear resistance on the design surface, a coating is formed by anodizing the design surface, which is the surface on the opposite side of the welded section.
In addition, in the case of housings 1 as shown in FIG. 3, a side member 3 and a cover member 2, which are both made from an aluminum alloy material, are integrally welded by friction stir welding to form a joint 5. The integrally-welded side member 3 and the cover member 2 are face milled to smoothen the outer surface of the welded side, including the welded section 4, and then a coating 6 is formed on the design surface by anodizing to improve corrosion and wear resistance properties.
However, color tone variations may occur in the coating 6 formed on the design surface due to differences of the crystal grain sizes between the portions corresponding to the welded section 4 and other non-welded portions.
Therefore, to eliminate color tone variations due to differences of crystal grain sizes between the portion corresponding to the welded section in the coating of the aluminum alloy welded component and other portions, it has been proposed to equalize the crystal grain sizes by performing a heat treatment prior to the anodizing treatment.
However, even if the crystal grain sizes are equalized by performing a heat treatment prior to anodizing, the color tone variations, which exist between the portion corresponding to the welded section in the coating of the aluminum alloy welded component and the other portions, may not be sufficiently reduced.
PRIOR ART DOCUMENTS
Patent Reference 1: Japanese Patent Application Publication No. 2003-225780
Patent Reference 2: Japanese Patent Application Publication No. 2003-230970
SUMMARY OF THE INVENTION
Therefore, the cross-sectional microstructures of the welded section obtained by friction stir welding and the other non-welded portions of the aluminum alloy welded component were first compared in detail using an optical microscope. As a result, it was found that second phase particles of 2 μm or larger in the welded section were decreased because the second phase particles made of coarse Al—Fe—Si particles were finely pulverized by the stirring; second phase particles of 5 μm or larger were scarcely found. Then, a comparison investigation was performed on the portion in the design surface that forms the coating, which is equivalent to the welded section (hereinafter, called “welded section equivalent portion”), and the other non-welded portions. As a result, it was found that the second phase particles, including the coarse second phase particles, were inhomogeneously dispersed in the welded section equivalent portion. In other words, due to the second phase particles being inhomogeneously dispersed in the welded section equivalent portion in this manner, color tone variations could be recognized in the coating, because variations in pit formation caused by etching during the anodizing treatment become larger.
Consequently, to eliminate color tone variations in the coating of the aluminum alloy welded component, it is necessary to promote a homogeneous dispersion of the second phase particles within the aluminum alloy welded component.
Therefore, color tone variations in the anodized coating of the aluminum alloy welded component attributable to the inhomogeneous dispersion of second phase particles at the welded section equivalent portion are preferably eliminated in the manner that will be further described below.
According to a first aspect of the present teachings, an aluminum alloy welded component is formed from one or more aluminum alloy members comprised of Mg: 0.3% to 6.0% (mass %, hereinafter the same), Cu: 0.2% or less, Si: 0.1% or less, Fe: 0.1% or less, the balance being Al and inevitable impurities. The grain size of second phase particles dispersed within the aluminum alloy member(s) is 5 μm or less when observed with an optical microscope. In addition, mutually-facing end surfaces of the aluminum alloy member(s) are integrally welded by friction stir welding so as to form a welded section, and a coating is formed by anodizing a surface of the welded section, or an opposite surface thereof. Because the amounts of Si and Fe that could form second phase particles, and the average diameter of the second phase particles, within the aluminum alloy member(s) fall within prescribed ranges, the inhomogeneous dispersion of the second phase particles is suppressed, even if the aluminum alloy member(s) is (are) welded in the welded section equivalent portion by friction stir welding and even as compared to the other portions. As a result, because variations in pit formation caused by etching during anodizing between the welded section equivalent portion and the other portions decrease, it is possible to prevent color tone variations in the coating of the aluminum alloy welded component.
In the context of the present teachings, Mg contained in the aluminum alloy welded component contributes to adjusting the strength of vehicular wheels and housings, which are shown in FIGS. 1-3. Therefore, because the strength is insufficient with less than 0.3% Mg and shaping becomes difficult with more than 6.0% Mg, while Mg should preferably be 0.3% to 6.0%, for a good balance of ensuring strength and ease of shaping, it is more preferably 1.0% to 6.0%, and even more preferably 2.0% to 6.0%.
In addition, Cu contributes to homogenizing the color tone of the entire coating after anodizing. Therefore, because the coating after anodizing will be turbid with more than 0.2% Cu due to the effect of fine precipitates of Al—Cu particles, 0.2% or less Cu is included according to the present invention.
Further, Si and Fe form second phase particles made of Al—Fe—Si. If the amounts of Si and Fe are each more than 0.1%, coarse second phase particles of Al—Fe—Si that exceed a grain size of 5 μm can easily form. Therefore, although the coarse second phase particles are preferably pulverized in the welded section during friction stir welding, the second phase particles, including the coarse particles, are inhomogeneously dispersed in the welded section equivalent portion by the agitation of the friction stir welding. As a result, variations in pit formation caused by the etching during anodizing increase due to the second phase particles being inhomogeneously dispersed in the welded section equivalent portion as compared to other portions, and color tone variations in the coating are caused. Therefore, according to the present teachings, the amounts of Si and Fe are each preferably 0.1% or less and more preferably 0.07% or less.
According to a second aspect of the present teachings, which is based on the above-described first aspect, the second phase particles within the aluminum alloy member(s) are dispersed in the aluminum alloy welded component in an amount of 10000 particles/mm2 or less when observed using an optical microscopic. If the second phase particles dispersed within the aluminum alloy members are thus reduced, the dispersion of the second phase particles in the welded section equivalent portion caused by the agitation during the friction stir welding can be minimized as compared to the other portions. As a result, variations in pit formation caused by the etching during anodizing become less, and the color tone variation in the coating can be eliminated more reliably.
As described so far, the inhomogeneous dispersion of the second phase particles is a cause of the color tone variation in the coating formed by anodizing the above-described aluminum alloy welded component. Therefore, if the distribution density of the second phase particles when observed using an optical microscope is greater than 10000 particles/mm2, the dispersion of the second phase particles in the welded section equivalent portion during friction stir welding becomes more inhomogeneous as compared to the other portions. Therefore, variations in pit formation caused by the etching during anodizing increasingly cause color tone variations in the coating. Thus, according to this aspect of the present teachings, the quantity of second phase particles is reduced to prevent their inhomogeneous dispersion in the welded section equivalent portion, and the distribution density of the second phase particles when observed using an optical microscope is set to 10000 particles/mm2 or less.
According to the aluminum alloy welded component of the present teachings, even though an anodized coating is formed on the side of the welded section surface or the surface opposite thereof, a higher quality anodized product can be achieved by limiting the amounts of metal(s) that may form second phase particles and by limiting the grain size of the second phase particles in both the welded section equivalent portion and the other portions. A uniform coating is thus formed that reliably eliminates color tone variations caused by the inhomogeneous dispersion of the second phase particles. Further, by appropriately setting the distribution density of the second phase particles, the elimination of color tone variations preferably can be achieved more reliably.
BRIEF DESCRIPTION OF THE DRAWINGS
FIGS. 1 and 2 show a process for making a vehicle wheel.
FIG. 3 shows a housing having an anodized coating.
DETAILED DESCRIPTION OF THE INVENTION
The objective, i.e. to eliminate color tone variations existing between the welded section equivalent portion and the other portions in the coating of the aluminum alloy welded component welded by friction stir welding, is realized by limiting the amounts of Si and Fe that form second phase particles, and by limiting the grain sizes of the second phase particles. Further, by preferably also limiting the distribution density of the second phase particles, the objective can be realized in a more reliable manner.
EXAMPLES
Therefore, the effects of the present teachings were confirmed by the following experimental results.
First, with respect to the aluminum alloy members, all of which contain Si and Fe that form second phase particles, two different 5000-series aluminum alloys were used as inventive materials 1, 2, and 3, in which the amounts of Si or Fe were at almost upper thresholds thereof. Two different 5052 materials, in which the amounts of Si or Fe slightly exceeded the upper thresholds, which will be called 5052 Material 1 and 5052 Material 2, were used as comparative examples.
The chemical compositions of the inventive materials 1, 2 and 3 and the 5052 Materials 1 and 2 are shown below in Table 1.
The inventive examples and the comparative examples were obtained by producing an ingot according to a semi-continuous casting process, homogenizing, forming plates having a thickness of 2.5 mm by hot rolling and cold rolling and then annealing to the O-temper (full-softening material). Two plates each having a size of 100 mm in width×200 mm in length were prepared. Longitudinal end surfaces thereof were butted with each other and friction stir welded. The tool revolutions per minute were 500 rpm, the welding speed was 800 mm/min., the tool shoulder diameter was 7 mm, and the probe diameter was 3 mm.
TABLE 1
(mass %)
Material Si Fe Cu Mn Mg Cr Zn Ti Al
Material 0.08 0.07 0.12 0.00 5.89 0.01 0.00 0.00 Bal.
1
Material 0.09 0.02 0.16 0.00 3.87 0.01 0.00 0.00 Bal.
2
Material 0.03 0.10 0.07 0.00 3.17 0.01 0.00 0.00 Bal.
3
5052 0.12 0.07 0.02 0.02 2.44 0.21 0.01 0.02 Bal.
Material
1
5052 0.04 0.13 0.05 0.03 2.61 0.19 0.02 0.01 Bal.
Material
2
Then, the longitudinal end surfaces of the aluminum alloy members of the inventive materials 1, 2, and 3 serving as examples of the present invention, as well as the 5052 Materials 1 and 2 serving as the comparative examples, were integrally welded by friction stir welding along abutted portions to form a welded section; after welding, 0.5 mm of the surface layer of the welded surface, including the welded section, was removed using a milling machine, then a rough surface finish was prepared by shot blasting and an anodized coating having a thickness of 10 μm was formed by anodizing with sulfuric acid.
As a result, the effect of the invention was confirmed as no color tone variation between the welded section equivalent portion and the other portions was observed in the coatings formed on the aluminum alloy welded components of the materials 1, 2, and 3 according to the examples of the present invention. On the other hand, color tone variations between the welded section equivalent portion and the other portions were apparent in the coatings formed on the aluminum alloy welded components of the 5052 Materials 1 and 2 according to the comparative examples.
Furthermore, surface microstructures were observed after removal of 0.5 mm by face milling in the welded section equivalent portion and the other portions of the inventive materials 1, 2, and 3 according to the examples of the invention and the 5052 Materials 1 and 2 of the comparative examples. After buffing and then etching with 5% hydrogen fluoride, the microstructures were magnified 400 times using an optical microscope, and the number of particles per 1 mm2 was obtained by measuring using an image analysis at 1 μm dot pitch grain size.
As a result, in the exemplary aluminum alloy welded components of the present invention, it was observed that the second phase particles were homogeneously dispersed in the welded section equivalent portion on the opposite surface as compared to the other portions. Furthermore, in inventive material 1, the largest particle diameter was 5 μm, and the distribution density of the second phase particles equal to 5 μm or smaller was 7350 particles/mm2; in inventive material 2, the largest particle diameter was 4 μm, and the distribution density of the second phase particles equal to 4 μm or smaller was 2310 particles/mm2; in inventive material 3, the largest particle diameter was 5 μm, and the distribution density of the second phase particles equal to 5 μm or smaller was 4150 particles/mm2. On the other hand, in the aluminum alloy welded components for the 5052 Materials according to the comparative examples, the second phase particles were inhomogeneously dispersed in the welded section equivalent portion as compared to the other portions. In addition, in 5052 Material 1, the largest particle diameter was 6 μm, and the distribution density of the second phase particles equal to 6 μm or smaller was 6170 particles/mm2; in 5052 Material 2, the largest particle diameter was 7 μm, and the distribution density of the second phase particles equal to 7 μm or smaller was 8620 particles/mm2.
In addition, the effect of appropriately setting the distribution density was confirmed by the following experiment.
Inventive material 4 was used as the inventive material and 5052 Material 3 containing a greater amount of Fe was used as the 5052 Material (comparative example). The chemical compositions are shown below in Table 2. The materials for testing were produced and evaluated by the same production and evaluation methods as mentioned above.
As a result, inventive material 4 exhibited neither color tone variations nor streak patterns in the welded section equivalent portion after the anodizing, the largest particle diameter was 4 μm, and the distribution density of the second phase particles equal to 4 μm or smaller was 2390 particles/mm2. On the other hand, the 5052 Material 3 exhibited color tone variations in the welded section equivalent portion after anodizing, the second phase particles were inhomogeneously dispersed in the welded section equivalent portion thereof as compared to the other portions, the largest particle diameter was 8 μm, and the distribution density of the second phase particles equal to 8 μm or smaller was 11670 particles/mm2.
TABLE 2
(mass %)
Material Si Fe Cu Mn Mg Cr Zn Ti Al
Material 0.04 0.07 0.08 0.00 3.25 0.01 0.00 0.00 Bal.
4
5052 0.09 0.28 0.03 0.01 2.52 0.18 0.01 0.01 Bal.
Material
3

Claims (20)

The invention claimed is:
1. An aluminum alloy welded component including:
one or more aluminum alloy members comprised of Mg: 0.3 mass % to 6.0 mass %, Cu: 0.2 mass % or less, Si: 0.1 mass % or less, Fe: 0.1 mass % or less, the balance being Al and inevitable impurities, wherein:
all second phase particles dispersed within the aluminum alloy member(s) have a grain size of 5 μm or less as observed with an optical microscope;
mutually-facing end surfaces of the aluminum alloy member(s) are integrally welded together along a friction stir weld that defines a welded section; and
an anodized coating is disposed on an outer surface of the welded section, or on an opposite surface thereof.
2. The aluminum alloy welded component according to claim 1, wherein the second phase particles are dispersed in the aluminum alloy members in an amount of 10000 particles/mm2 or less as observed with an optical microscope.
3. The aluminum alloy welded component according to claim 2, wherein the aluminum alloy member(s) contain(s) 1.0-6.0 mass % Mg.
4. The aluminum alloy welded component according to claim 3, wherein the aluminum alloy member(s) contain(s) 2.0-6.0 mass % Mg.
5. The aluminum alloy welded component according to claim 4, wherein the aluminum alloy member(s) contain(s) 0.07 mass % or less Si and 0.07 mass % or less Fe.
6. The aluminum alloy welded component according to claim 5, wherein the aluminum alloy welded component is a vehicular wheel comprising a single cylindrical-shaped aluminum alloy member having a friction stir weld along its mutually-facing end surfaces.
7. The aluminum alloy welded component according to claim 5, wherein the aluminum alloy welded component is a housing comprising two aluminum alloy members having a friction stir weld along their mutually-facing end surfaces.
8. The aluminum alloy welded component according to claim 1, wherein the aluminum alloy member(s) contain(s) 1.0-6.0 mass % Mg.
9. The aluminum alloy welded component according to claim 8, wherein the aluminum alloy member(s) contain(s) 2.0-6.0 mass % Mg.
10. The aluminum alloy welded component according to claim 1, wherein the aluminum alloy member(s) contain(s) 0.07 mass % or less Si and 0.07 mass % or less Fe.
11. The aluminum alloy welded component according to claim 1, wherein the aluminum alloy welded component is a vehicular wheel comprising a single cylindrical-shaped aluminum alloy member integrally welded having a friction stir weld along its mutually-facing end surfaces.
12. The aluminum alloy welded component according to claim 1, wherein the aluminum alloy welded component is a housing comprising two aluminum alloy members having a friction stir weld along their mutually-facing end surfaces.
13. A method for manufacturing an aluminum alloy welded component, including:
abutting mutually-facing end surfaces of one or more aluminum alloy members comprised of 0.3-6.0 mass % Mg, 0.2 mass % or less Cu, 0.1 mass % or less Si, 0.1 mass % or less Fe, the balance being Al and inevitable impurities, wherein all second phase particles dispersed within the aluminum alloy member(s) have a grain size of 5 μm or less as observed with an optical microscope,
friction stir welding along the abutted mutually-facing end surfaces to integrally weld them together and form a welded section; and
anodizing an outer surface of the welded section, or an opposite surface thereof, to form an anodized coating thereon.
14. The method according to claim 13, wherein the anodizing step is performed with sulfuric acid.
15. The method according to claim 14, wherein the anodized step is performed until the anodized coating has a thickness of 10 μm.
16. The method according to claim 13, wherein the anodized step is performed until the anodized coating has a thickness of 10 μm.
17. An aluminum alloy welded component produced by the method of claim 13.
18. An aluminum alloy welded component including:
one or more aluminum alloy members comprised of Mg: 0.3 mass % to 6.0 mass %, Cu: 0.2 mass % or less, Si: 0.1 mass % or less, Fe: 0.1 mass % or less, the balance being Al and inevitable impurities, wherein:
second phase particles dispersed within the aluminum alloy member(s) have a grain size of 5 μm or less as observed with an optical microscope;
mutually-facing end surfaces of the aluminum alloy member(s) are integrally welded by friction stir welding so as to form a welded section; and
a coating is formed by anodizing an outer surface of the welded section, or on an opposite surface thereof.
19. The aluminum alloy welded component according to claim 18, wherein the second phase particles are dispersed in the aluminum alloy members in an amount of 10000 particles/mm2 or less as observed with an optical microscope.
20. The aluminum alloy welded component according to claim 19, wherein the aluminum alloy member(s) contain(s) 2.0-6.0 mass % Mg, 0.07 mass % or less Si and 0.07 mass % or less Fe.
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US20150030379A1 (en) * 2013-07-25 2015-01-29 Apple Inc. Solid state deposition methods, apparatuses, and products

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Citations (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH028342A (en) 1988-06-28 1990-01-11 Sky Alum Co Ltd Aluminum alloy plate for two-piece wheel rim and its manufacture
JPH1121648A (en) 1997-07-04 1999-01-26 Mitsubishi Alum Co Ltd Aluminum material with brightness characteristic, and its production
JPH11285862A (en) 1998-04-03 1999-10-19 Nippon Light Metal Co Ltd Aluminum structural body excellent in surface treatment property, and its manufacture
JP2000248399A (en) 1999-02-26 2000-09-12 Kobe Steel Ltd Aluminum or aluminum alloy member, vacuum vessel and reaction vessel having excellent corrosion resistance
JP2001269780A (en) 2000-03-27 2001-10-02 Ishikawajima Harima Heavy Ind Co Ltd Container for cryogenic liquefied gas
US20010050118A1 (en) * 1995-02-24 2001-12-13 Guy-Michel Raynaud Product for a welded construction made of almgmn alloy having improved mechanical strength
US20020006352A1 (en) * 2000-03-31 2002-01-17 Spanjers Martinus Godefridus Johannes Aluminium die-casting alloy
US6516992B1 (en) 1996-05-31 2003-02-11 The Boeing Company Friction stir welding with simultaneous cooling
US20030145912A1 (en) * 1998-02-20 2003-08-07 Haszler Alfred Johann Peter Formable, high strength aluminium-magnesium alloy material for application in welded structures
JP2003225780A (en) 2002-01-30 2003-08-12 Nippon Light Metal Co Ltd Aluminum based structure and production method therefor
JP2003230970A (en) 2002-02-14 2003-08-19 Sumitomo Light Metal Ind Ltd Aluminum alloy made rim in wheel for vehicle and manufacturing method thereof
US20030160085A1 (en) 2002-02-26 2003-08-28 Applied Materials, Inc. Plasma-resistant, welded aluminum structures for use in semiconductor apparatus
US20030205479A1 (en) 2002-02-08 2003-11-06 Yixing Lin Halogen-resistant, anodized aluminium for use in semiconductor processing apparatus
US20040041005A1 (en) 2001-09-25 2004-03-04 Sumitomo Light Metal Industries, Ltd. Method of manufacturing tubular body, by friction stir welding
US20040084506A1 (en) 2002-11-05 2004-05-06 Sumitomo Light Metal Industries, Ltd. Method of joining together two planar members by friction stir welding, and tab plate used in the same method
JP2004176154A (en) 2002-11-28 2004-06-24 Kobe Steel Ltd Aluminum alloy sheet for wheel, production method therefor, wheel produced by using the same, and production method for the wheel
JP2005000967A (en) 2003-06-13 2005-01-06 Sumitomo Light Metal Ind Ltd Aluminum alloy-made rim of wheel for vehicle and manufacturing method thereof
US20050037188A1 (en) * 2002-09-25 2005-02-17 Pechiney Rhenalu Composite laminated aluminum-glass fiber sandwich panels
JP2006043730A (en) 2004-08-04 2006-02-16 Honda Motor Co Ltd Friction stir joining method
US20060278325A1 (en) 2005-06-09 2006-12-14 Sumitomo Light Metal Industries, Ltd. Method of joining together end portions of superposed members
JP2007061877A (en) 2005-09-01 2007-03-15 Sumitomo Light Metal Ind Ltd Method of manufacturing cylindrical article
JP2007064129A (en) 2005-09-01 2007-03-15 Nissan Motor Co Ltd Piston for internal combustion engine and method for manufacturing same
US20070102071A1 (en) * 2005-11-09 2007-05-10 Bac Of Virginia, Llc High strength, high toughness, weldable, ballistic quality, castable aluminum alloy, heat treatment for same and articles produced from same
US20070102822A1 (en) 2003-12-18 2007-05-10 Takashi Kubota Aluminum base target and process for producing the same
US20070138235A1 (en) 2005-12-15 2007-06-21 Sumitomo Light Metal Industries, Ltd. Method of joining aluminum alloy members and joined product used for press forming
US20070138239A1 (en) 2005-12-15 2007-06-21 Sumitomo Light Metal Industries, Ltd. Method of joining heat-treatable aluminum alloy members by friction stir welding and joined product obtained by the method and used for press forming
JP2007275396A (en) 2006-04-10 2007-10-25 Sumitomo Light Metal Ind Ltd Aluminum alloy bat, and method of connecting grip end of the aluminum alloy bat
US20080274383A1 (en) 2004-04-08 2008-11-06 Showa Denko K.K. Process for Fabricating Pressure Vessel Liner
US20100051147A1 (en) 2003-04-07 2010-03-04 The Society Of Japanese Aerospace Companies High-strength aluminum alloy extruded product exhibiting excellent corrosion resistance and method of manufacturing same
US20100170996A1 (en) * 2009-01-07 2010-07-08 Sankaran Krishnan K Weldable high-strength aluminum alloys
JP2011025275A (en) 2009-07-24 2011-02-10 Sumitomo Light Metal Ind Ltd Method for joining aluminum alloy material and aluminum alloy panel manufactured by the method for joining the same
US7993575B2 (en) 2000-05-08 2011-08-09 Megastir Technologies, LLC Friction stir welding using a superabrasive tool
US20110236718A1 (en) 2009-06-05 2011-09-29 Sumitomo Light Metal Industries, Ltd. Frame member for use in two-wheeled vehicle and all-terrain vehicle, and method for producing the same
US20140023874A1 (en) 2012-07-18 2014-01-23 Sumitomo Light Metal Industries, Ltd. Method for welding aluminum alloy materials and aluminum alloy panel produced thereby

Patent Citations (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH028342A (en) 1988-06-28 1990-01-11 Sky Alum Co Ltd Aluminum alloy plate for two-piece wheel rim and its manufacture
US20010050118A1 (en) * 1995-02-24 2001-12-13 Guy-Michel Raynaud Product for a welded construction made of almgmn alloy having improved mechanical strength
US6516992B1 (en) 1996-05-31 2003-02-11 The Boeing Company Friction stir welding with simultaneous cooling
JPH1121648A (en) 1997-07-04 1999-01-26 Mitsubishi Alum Co Ltd Aluminum material with brightness characteristic, and its production
US20030145912A1 (en) * 1998-02-20 2003-08-07 Haszler Alfred Johann Peter Formable, high strength aluminium-magnesium alloy material for application in welded structures
JPH11285862A (en) 1998-04-03 1999-10-19 Nippon Light Metal Co Ltd Aluminum structural body excellent in surface treatment property, and its manufacture
JP2000248399A (en) 1999-02-26 2000-09-12 Kobe Steel Ltd Aluminum or aluminum alloy member, vacuum vessel and reaction vessel having excellent corrosion resistance
JP2001269780A (en) 2000-03-27 2001-10-02 Ishikawajima Harima Heavy Ind Co Ltd Container for cryogenic liquefied gas
US20020006352A1 (en) * 2000-03-31 2002-01-17 Spanjers Martinus Godefridus Johannes Aluminium die-casting alloy
US8302834B2 (en) 2000-05-08 2012-11-06 MegaStar Technologies LLC Friction stir welding using a superabrasive tool
US7993575B2 (en) 2000-05-08 2011-08-09 Megastir Technologies, LLC Friction stir welding using a superabrasive tool
US20040041005A1 (en) 2001-09-25 2004-03-04 Sumitomo Light Metal Industries, Ltd. Method of manufacturing tubular body, by friction stir welding
JP2003225780A (en) 2002-01-30 2003-08-12 Nippon Light Metal Co Ltd Aluminum based structure and production method therefor
US20030205479A1 (en) 2002-02-08 2003-11-06 Yixing Lin Halogen-resistant, anodized aluminium for use in semiconductor processing apparatus
JP2003230970A (en) 2002-02-14 2003-08-19 Sumitomo Light Metal Ind Ltd Aluminum alloy made rim in wheel for vehicle and manufacturing method thereof
CN1638910A (en) 2002-02-26 2005-07-13 应用材料有限公司 Plasma-resistant, welded aluminum structures for use in semiconductor processing apparatus
US20030160085A1 (en) 2002-02-26 2003-08-28 Applied Materials, Inc. Plasma-resistant, welded aluminum structures for use in semiconductor apparatus
CN101064243A (en) 2002-02-26 2007-10-31 应用材料有限公司 Semiconductor processing apparatus including complex-shaped friction welded aluminum structures
WO2003073478A2 (en) 2002-02-26 2003-09-04 Applied Materials, Inc. Plasma-resistant, welded aluminum structures for use in semiconductor processing apparatus
US20040041004A1 (en) 2002-02-26 2004-03-04 Applied Materials, Inc. Semiconductor processing apparatus including plasma-resistant, welded aluminum structures
US20050037188A1 (en) * 2002-09-25 2005-02-17 Pechiney Rhenalu Composite laminated aluminum-glass fiber sandwich panels
US20040084506A1 (en) 2002-11-05 2004-05-06 Sumitomo Light Metal Industries, Ltd. Method of joining together two planar members by friction stir welding, and tab plate used in the same method
JP2004176154A (en) 2002-11-28 2004-06-24 Kobe Steel Ltd Aluminum alloy sheet for wheel, production method therefor, wheel produced by using the same, and production method for the wheel
US20100051147A1 (en) 2003-04-07 2010-03-04 The Society Of Japanese Aerospace Companies High-strength aluminum alloy extruded product exhibiting excellent corrosion resistance and method of manufacturing same
US20090250144A1 (en) 2003-06-09 2009-10-08 Sumitomo Light Metal Industries, Ltd. Method of joining heat-treatable aluminum alloy members by friction stir welding
JP2005000967A (en) 2003-06-13 2005-01-06 Sumitomo Light Metal Ind Ltd Aluminum alloy-made rim of wheel for vehicle and manufacturing method thereof
US20070102822A1 (en) 2003-12-18 2007-05-10 Takashi Kubota Aluminum base target and process for producing the same
US20080274383A1 (en) 2004-04-08 2008-11-06 Showa Denko K.K. Process for Fabricating Pressure Vessel Liner
JP2006043730A (en) 2004-08-04 2006-02-16 Honda Motor Co Ltd Friction stir joining method
US20060278325A1 (en) 2005-06-09 2006-12-14 Sumitomo Light Metal Industries, Ltd. Method of joining together end portions of superposed members
JP2007061877A (en) 2005-09-01 2007-03-15 Sumitomo Light Metal Ind Ltd Method of manufacturing cylindrical article
JP2007064129A (en) 2005-09-01 2007-03-15 Nissan Motor Co Ltd Piston for internal combustion engine and method for manufacturing same
US20070102071A1 (en) * 2005-11-09 2007-05-10 Bac Of Virginia, Llc High strength, high toughness, weldable, ballistic quality, castable aluminum alloy, heat treatment for same and articles produced from same
US20070138239A1 (en) 2005-12-15 2007-06-21 Sumitomo Light Metal Industries, Ltd. Method of joining heat-treatable aluminum alloy members by friction stir welding and joined product obtained by the method and used for press forming
US20070138235A1 (en) 2005-12-15 2007-06-21 Sumitomo Light Metal Industries, Ltd. Method of joining aluminum alloy members and joined product used for press forming
JP2007275396A (en) 2006-04-10 2007-10-25 Sumitomo Light Metal Ind Ltd Aluminum alloy bat, and method of connecting grip end of the aluminum alloy bat
US20100170996A1 (en) * 2009-01-07 2010-07-08 Sankaran Krishnan K Weldable high-strength aluminum alloys
US20110236718A1 (en) 2009-06-05 2011-09-29 Sumitomo Light Metal Industries, Ltd. Frame member for use in two-wheeled vehicle and all-terrain vehicle, and method for producing the same
JP2011025275A (en) 2009-07-24 2011-02-10 Sumitomo Light Metal Ind Ltd Method for joining aluminum alloy material and aluminum alloy panel manufactured by the method for joining the same
US20140023874A1 (en) 2012-07-18 2014-01-23 Sumitomo Light Metal Industries, Ltd. Method for welding aluminum alloy materials and aluminum alloy panel produced thereby

Non-Patent Citations (6)

* Cited by examiner, † Cited by third party
Title
English translation of International Preliminary Report on Patentability from parent PCT application No. PCT/JP2010/068226.
Extended European Search Report from the European Patent Office in counterpart European patent application No. 10858158.8 mailed on Mar. 9, 2015, including European Search Opinion, European Search Report and examined claims 1-9.
Final Office Action mailed Jul. 31, 2013 in related U.S. Appl. No. 13/552,394.
International Search Report from parent PCT application No. PCT/JP2010/068226.
Office Action from Chinese Patent Office mailed Jan. 6, 2015 in counterpart Chinese Application No. 201080065641.5.
U.S. Appl. No. 13/552,394, filed Jul. 18, 2012.

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150030379A1 (en) * 2013-07-25 2015-01-29 Apple Inc. Solid state deposition methods, apparatuses, and products
US9951425B2 (en) * 2013-07-25 2018-04-24 Apple Inc. Solid state deposition methods, apparatuses, and products

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